Browse Standards AIR5826A
Historical REVISED 2016-10-13

Distortion Synthesis/Estimation Techniques AIR5826A

This document provides a review of published methods that have been used to provide estimates of the levels of distortion and/or the concomitant loss of stability pressure ratio that can occur when the recommended full complement of aerodynamic interface plane high-response instrumentation is not used when obtaining inlet data. The methods have been categorized based on the underlying mathematical representation of the aerophysics. Further, the use of maximum value statistics, which has been used to further improve the results where short-duration time records have been employed, is discussed.
AIR5826B
2017-03-21
Latest
Stabilized
AIR5826A
2016-10-13
Historical
Revised
AIR5826
2011-07-20
Historical
Reaffirmed

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